*HEADING
: NAFEMS TEST LE2, Cylindrical Shell Bending Patch Test  [S9R5]
*NODE
 1, 1.0, 0.0, 0.0, 1.0, 0.0, 0.0
 5, 1.0, 30.0, 0.0, 1.0, 0.0, 0.0
 21,1.0, 0.0, 0.5, 1.0, 0.0, 0.0
 25,1.0, 30.0, 0.5, 1.0, 0.0, 0.0
 13,1.0, 20.0, 0.3, 1.0, 0.0, 0.0
*NGEN,NSET=EDGEAB
 1,21,5
*NGEN,NSET=EDGECD
 5,25,5
*NGEN,NSET=EDGEAD
 1,5
*NGEN,NSET=EDGEBC
 21,25,
*NGEN
 11,13
 13,15
 3,13,5
 13,23,5
 6,8
 8,10
 16,18
 18,20
*NSET,NSET=NALL,GEN
 1,25
*NMAP,NSET=NALL,TYPE=CYLINDRICAL
0.,0.,0.,0.,0.,1.
1.,0.,0.
*ELEMENT,TYPE=S9R5,ELSET=ALLELS
 1,1,3,13,11, 2,8,12,6,7
*ELGEN,ELSET=ALLELS
 1,2,2,1,2,10,10
*MATERIAL,NAME=MAT
*ELASTIC,TYPE=ISOTROPIC
2.1E5,0.3
*orientation, name=ori, system=cylindrical
 0.,0.,0., 0.,0.,1.
 1,0.
*SHELL SECTION,MATERIAL=MAT,ELSET=ALLELS, orientation=ori
0.01, 
*TRANSFORM,TYPE=C,NSET=NALL
0.,0.,0.,0.,0.,1.
*BOUNDARY
 EDGEAD,ZSYMM
 EDGEBC,ZSYMM
 EDGEAB,1,6
*RESTART,WRITE
*STEP
*STATIC
*CLOAD
 5,6,0.041667E3
 10,6,0.166667E3
 15,6,0.083333E3
 20,6,0.166667E3
 25,6,0.041667E3
*EL PRINT,POS=AVERAGED AT NODES
S, 
*EL FILE,POS=AVERAGED AT NODES
S, 
*END STEP